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1.1 This specification establishes the airworthiness design standards associated with aeroplane weight and center of gravity.
1.2 The term “aeroplane” is utilized in this specification as it was originally conceived for normal category fixed wing aircraft with a maximum certificated weight of 19 000 lb or less and a passenger seating configuration up to 19 as defined in the Rules. However, these standards may be more broadly applicable and their usage should not be unnecessarily limited.
1.3 The applicant for a design approval shall seek the individual guidance of their respective civil aviation authority (CAA) body concerning the use of this specification as part of a certification plan. For information on which CAA regulatory bodies have accepted this specification (in whole or in part) as a means of compliance to their small aircraft airworthiness regulations (hereinafter referred to as “the Rules”), refer to ASTM Committee F44 webpage (www.astm.org/COMMITTEE/F44.htm), which includes CAA website links.
1.4 Units—The values stated in either SI units or inch-pound units are to be regarded separately as standard. The values stated in each system may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the two systems may result in non-conformance with the standard.
1.5 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use.
1.6 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
2. Referenced Documents (purchase separately) The documents listed below are referenced within the subject standard but are not provided as part of the standard.
F3060 Terminology for Aircraft
F3061 Specification for Systems and Equipment in Small Aircraft
F3063/F3063M Specification for Design and Integration of Fuel/Energy Storage and Delivery System Installations for Aeroplanes
F3120 Specification for Ice Protection for General Aviation Aircraft
F3174/F3174M Specification for Establishing Operating Limitations and Information for Aeroplanes
ICS Number Code 49.020 (Aircraft and space vehicles in general)
UNSPSC Code 25130000(Aircraft)
|Link to Active (This link will always route to the current Active version of the standard.)|
ASTM F3082 / F3082M-17, Standard Specification for Weights and Centers of Gravity of Aircraft, ASTM International, West Conshohocken, PA, 2017, www.astm.orgBack to Top